Air Tractor AT-401 Safety Record
Complete NTSB accident and incident history. 73 events recorded from 1989 to 2014.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Aug 12, 2008 | Ida Grove, IA | N45029 | Incident | substantial |
A failure of the turbocharger blower which resulted in the partial loss of power. Factors associated with the accident were the low altitude of the a…A failure of the turbocharger blower which resulted in the partial loss of power. Factors associated with the accident were the low altitude of the airplane and the embankment. |
| Jun 06, 2007 | Oak Grove, LA | N92PK | Incident | substantial |
A complete loss of power due to failure of the impeller drive gear train and displacement of the blower spring drive mechanism, which resulted in seiz…A complete loss of power due to failure of the impeller drive gear train and displacement of the blower spring drive mechanism, which resulted in seizure of the propeller shaft/crankshaft. Also causal was the failure of the phenolic separator bracket of the rear impeller support bearing for undetermined reasons. A factor was the none suitable terrain for the forced landing. |
| Jun 03, 2006 | Victoria, TX | N9190B | Incident | substantial | The pilot's delay in aborting the takeoff which resulted in an overrun. A contributing factor was the unfavorable wind. |
| Jun 01, 2006 | Garden City, TX | N7318C | Incident | substantial |
The pilot's improper in-flight planning resulting in the loss of engine power due to fuel exhaustion. A contributing factor was the lack of suitable …The pilot's improper in-flight planning resulting in the loss of engine power due to fuel exhaustion. A contributing factor was the lack of suitable terrain for the forced landing. |
| Aug 19, 2005 | Winnie, TX | N4545W | Incident | minor | The loss of engine power due to the failure of the second-stage turbine wheel as a result of low cycle fatigue. |
| Feb 04, 2005 | Calexico, CA | N4530L | Incident | substantial | a loss of directional control due to a jammed rudder pedal, which prevented the pilot from exercising full rudder control authority. |
| Jul 10, 2004 | Winnsboro, LA | N10061 | Incident | substantial | The pilot's mismanagement of fuel resulting in fuel starvation. A contributing factor was the ditch. |
| Jun 23, 2004 | Britton, SD | N1013N | Incident | substantial |
The loss of engine power due to a stuck exhaust valve and the unsuitable terrain encountered during the forced landing. A factor to the accident was …The loss of engine power due to a stuck exhaust valve and the unsuitable terrain encountered during the forced landing. A factor to the accident was the soft terrain condition. |
| May 19, 2004 | San Angelo, TX | N4508Y | Incident | destroyed | The loss of engine power for undetermined reasons. A contributing factor was the soft terrain encountered during the aborted takeoff. |
| Jul 22, 2002 | Pratt, KS | N60747 | Incident | substantial | The pilot's failure to maintain terrain clearance. A factor was low altitude flight. |
| Nov 30, 2001 | Las Vegas, NV | N9186J | Incident | substantial |
the failure of the AT-401 pilot to maintain clearance with the AT-402 airplane during landing. Contributing factors were the unreliable communication…the failure of the AT-401 pilot to maintain clearance with the AT-402 airplane during landing. Contributing factors were the unreliable communication radio in the AT-401, the AT-401 pilot's continued flight with known communication radio problems, and the glare of the sun. |
| Aug 09, 2001 | Grand Coteau, LA | N10140 | Incident | substantial |
the loss of engine power while maneuvering, which resulted from a fractured #4 cylinder head at the exhaust valve rocker arm boss. A contributing fac…the loss of engine power while maneuvering, which resulted from a fractured #4 cylinder head at the exhaust valve rocker arm boss. A contributing factor was the lack of suitable terrain for the forced landing. |
| Jul 27, 2001 | Kenesaw, NE | N4553K | Incident | minor |
The propeller blade fatigue leading to its tip separating during an aerial application. Factors were no suitable terrain for an emergency landing, hi…The propeller blade fatigue leading to its tip separating during an aerial application. Factors were no suitable terrain for an emergency landing, high vegetation, and soft terrain encountered during the emergency landing. |
| Jul 02, 2001 | Ellinwood, KS | N4549E | Incident | substantial | The pilot failed to see and avoid the guy wire during an aerial application flight. A factor associated with the accident was the guy wire. |
| May 12, 2001 | Warsaw, IL | N1008Q | Incident | substantial |
the rocker assembly failure during low level maneuvering. Factors were the soft and sandy terrain and the unsuitable terrain the pilot encountered dur…the rocker assembly failure during low level maneuvering. Factors were the soft and sandy terrain and the unsuitable terrain the pilot encountered during the forced landing. |
| Aug 26, 2000 | SUPERIOR, NE | N91842 | Incident | destroyed | the cracked number 7 cylinder exhaust valve. A factor relating to this accident was the tree. |
| Jul 13, 2000 | RIPLEY, CA | N4508Y | Incident | substantial | A loss of engine power due to the separation of a connecting rod from the crankshaft. |
| Apr 22, 2000 | LAWRENCEBURG, TN | N6096P | Incident | substantial | The loss of engine power due to a stuck exhaust valve that resulted in the collision with a tree while maneuvering for the forced landing. |
| Jan 25, 2000 | RAYVILLE, LA | N91968 | Incident | substantial | The loss of engine power due to a crack in the #6 cylinder. A factor was the lack of suitable terrain for the forced landing. |
| Sep 13, 1999 | CALEDONIA, MS | N45205 | Incident | substantial | The failure of the fuel control gear train due to oil contamination. A factor was Inadequate maintenance. |
| Aug 12, 1999 | HUMPHREY, AR | N1031Q | Incident | substantial | Fuel exhaustion as a result of the pilot's failure to refuel the airplane. |
| Aug 02, 1999 | MOORE HAVEN, FL | N15585 | Incident | substantial |
The pilot exceeding the gross takeoff weight which reduced the climb capability and subsequent in-flight collision with terrain. Contributing to the …The pilot exceeding the gross takeoff weight which reduced the climb capability and subsequent in-flight collision with terrain. Contributing to the accident was the high temperature and the pilot's failure to use aircraft performance data for the weather conditions. |
| May 27, 1999 | JEROME, ID | N6024M | Incident | substantial | Fuel exhaustion. Carburetor contamination and rough terrain were factors. |
| Aug 28, 1998 | N. OTTAWA TWP., MN | N4543F | Incident | destroyed | A loss of engine power due to a worn piston ring. A related factor was the owner exceeded the manufacturer's recommended engine overhaul. |
| May 24, 1998 | RICH, MS | N1008Y | Incident | substantial | a loss of engine power for an undetermined reason, resulting in a forced landing and subsequent impact with rough terrain. |